| Citation: | ZHANG Kai, XIONG Jiajun, FU Tingting, et al. Multi-model estimation of HGV based on coupled aerodynamic parameters[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(10): 2156-2164. doi: 10.13700/j.bh.1001-5965.2018.0028(in Chinese)
|
Using aerodynamic parameters to model the unknown aerodynamics is an effective way to improve the tracking accuracy of hypersonic gliding vehicles. The aerodynamic acceleration and its derivative is analyzed to prove the necessity of unknown aerodynamics modeling in this paper. Based on the non-coupled aerodynamic parameter model, two coupled aerodynamic parameter models, the Bank model and the spiral model, are constructed by using the priori information of the aerodynamic acceleration in the turn and pitch directions. The target's state and aerodynamic parameters are estimated by a decomposed estimator, and the state filter and the aerodynamic parameter filter are deduced respectively. Meanwhile, considering the maneuver frequencies of parameters in different flight modes, the interacting multiple model tracking algorithm is built based on the coupled aerodynamic parameters. The simulation results show that the accuracy of the proposed algorithms is significantly higher than other tracking algorithms for such targets. In the meantime, the performance of the bank model is better than that of the spiral model, and its computational complexity is smaller.
| [1] |
PAUL L M, VINCENT L R, LUAT T N, et al.NASA hypersonic fight demonstration overview, status, and future plans[J].Acta Astronautica, 2004, 55(7):619-630. http://www.sciencedirect.com/science/article/pii/S0094576504001869
|
| [2] |
ACTON J M.Hypersonic boost-glide weapons[J].Science & Global Security, 2015, 23(3):191-219. http://d.old.wanfangdata.com.cn/NSTLQK/NSTL_QKJJ029569501/
|
| [3] |
BAR-SHALOM Y, LI X R, KIRUBARAJAN T.Estimation with applications to tracking and navigation[M].Hoboken:Wiley Interscience, 2001:121-176.
|
| [4] |
LI X R, JILKOV V P.Survey of maneuvering target tracking.Part Ⅰ:Dynamic models[J].IEEE Transactions on Aerospace and Electronic Systems, 2003, 39(4):1333-1364. doi: 10.1109/TAES.2003.1261132
|
| [5] |
LI X R, JILKOV V P.Survey of maneuvering target tracking. Part Ⅱ:Motion models of ballistic and space targets[J].IEEE Transactions on Aerospace and Electronic Systems, 2010, 46(1):96-119. doi: 10.1109/TAES.2010.5417150
|
| [6] |
KIM J, VADDI S S, MENON P K, et al.Comparison between nonlinear filtering techniques for spiraling ballistic missile state estimation[J].IEEE Transactions on Aerospace and Electronic Systems, 2012, 48(1):313-328. doi: 10.1109/TAES.2012.6129638
|
| [7] |
雍恩米, 钱炜祺, 何开锋.基于雷达跟踪仿真的滑翔式再入弹道突防性能分析[J].宇航学报, 2012, 33(10):1370-1376. doi: 10.3873/j.issn.1000-1328.2012.10.002
YONG E M, QIAN W Q, HE K F.Penetration ability analysis for glide reentry trajectory based on radar tracking[J].Journal of Astronautics, 2012, 33(10):1370-1376(in Chinese). doi: 10.3873/j.issn.1000-1328.2012.10.002
|
| [8] |
吴楠, 陈磊.高超声速滑翔再入飞行器弹道估计的自适应卡尔曼滤波[J].航空学报, 2013, 34(8):1960-1971. http://d.old.wanfangdata.com.cn/Periodical/hkxb201308023
WU N, CHEN L.Adaptive Kalman filtering for trajectory estimation of hypersonic glide reentry vehicles[J].Acta Aeronautica et Astronautica Sinica, 2013, 34(8):1960-1971(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hkxb201308023
|
| [9] |
张凯, 熊家军, 韩春耀, 等.一种基于气动力模型的高超声速滑翔目标跟踪算法[J].宇航学报, 2017, 38(2):123-130. doi: 10.3873/j.issn.1000-1328.2017.02.003
ZHANG K, XIONG J J, HAN C Y, et al.A tracking algorithm of hypersonic glide reentry vehicle via aerodynamic model[J].Journal of Astronautics, 2017, 38(2):123-130(in Chinese). doi: 10.3873/j.issn.1000-1328.2017.02.003
|
| [10] |
LEE S, LIU C.Trajectory estimation of reentry vehicles by use of on-line input estimator[J].Journal of Guidance, Control, and Dynamics, 1999, 22(6):808-815. doi: 10.2514/2.4482
|
| [11] |
周政, 刘进忙, 郭相科.基于随机模型近似的再入目标自适应跟踪算法[J].北京航空航天大学学报, 2014, 40(5):651-657. http://bhxb.buaa.edu.cn/CN/abstract/abstract12926.shtml
ZHOU Z, LIU J M, GUO X K.Adaptive tracking algorithm for reentry vehicle based on stochastic model approximation[J].Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(5):651-657(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract12926.shtml
|
| [12] |
LIANG Y Q, HAN C Z.Hybrid state estimation and model-set design of invariable-structure semi-ballistic reentry vehicle[J].Science China:Information Sciences, 2011, 54(4):812-823. doi: 10.1007/s11432-010-4159-6
|
| [13] |
秦雷, 李君龙, 周荻.基于交互式多模型算法跟踪临近空间目标[J].系统工程与电子技术, 2014, 36(7):1243-1249. http://d.old.wanfangdata.com.cn/Periodical/xtgcydzjs201407004
QIN L, LI J L, ZHOU D.Tracking for near space target based on IMM algorithm[J].Systems Engineering and Electronics, 2014, 36(7):1243-1249(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/xtgcydzjs201407004
|
| [14] |
OLIVIER D M, ROBERT H B.Tracking and identification of a maneuvering reentry vehicle[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit.Reston: AIAA, 2003: 1-11.
|
| [15] |
赵汉元.飞行器再入动力学与制导[M].长沙:国防科技大学出版社, 1997:23-97.
ZHAO H Y.Dynamics and guidance of vehicle entry[M].Changsha:National University of Defense Technology Press, 1997:23-97(in Chinese).
|
| [16] |
朱辉玉, 王刚, 孙泉华, 等.典型气动布局高超声速飞行的气动力数值评估[J].空气动力学学报, 2012, 30(3):365-372. doi: 10.3969/j.issn.0258-1825.2012.03.015
ZHU H Y, WANG G, SUN Q H, et al.Numerical evaluation on aerodynamic of typical hypersonic configurations for hypersonic flight[J].Acta Aerodynamica Sinica, 2012, 30(3):365-372(in Chinese). doi: 10.3969/j.issn.0258-1825.2012.03.015
|
| [17] |
战培国.美国陆军先进高超声速武器气动问题分析[J].航空科学技术, 2015, 26(1):7-11. doi: 10.3969/j.issn.1007-5453.2015.01.003
ZHAN P G.Aerodynamic analysis of US army advanced hypersonic weapon[J].Aeronautical Science & Technology, 2015, 26(1):7-11(in Chinese). doi: 10.3969/j.issn.1007-5453.2015.01.003
|
| [18] |
GHOSH S, MUKHOPADHYAY S.Tracking reentry ballistic targets using acceleration and jerk models[J].IEEE Transactions on Aerospace and Electronic Systems, 2011, 47(1):666-683. doi: 10.1109/TAES.2011.5705698
|
| [19] |
何友, 修建娟, 关欣, 等.雷达数据处理与应用[M].3版.北京:电子工业出版社, 2013:36-62.
HE Y, XIU J J, GUAN X, et al.Rader data processing with applications[M].3rd ed.Beijing:Publishing House of Electronics Industry, 2013:36-62(in Chinese).
|
| [20] |
PHILLIPS T H.A common aero vehicle (CAV) model, description, and employment guide[R/OL].[2013-12-12].http://www.dtic.Mil/matrics/sbir/sbir041/srch/af031a.doc.
|
Figures(6) / Tables(2)
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
DownLoad:
